- Owner type
- Co-owned, fractional ownership
- Serial number
- 20690
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 20, 2017
- Certificate issued
- February 28, 2023
- Expires
- February 28, 2030
- Mode S code
- A9EDE9
Bombardier BD-100-1A10TCDS T00005NYAirframe · Bombardier BD-100-1A10TCDS E00010LAEngine · Honeywell AS907-2-1A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2006 | 1 |
|---|---|
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 5 |
| 2018 | 4 |
| 2019 | 3 |
| 2020 | 3 |
| 2021 | 6 |
| 2022 | 5 |
| 2023 | 9 |
| 2024 | 8 |
| 2025 | 1 |
| 2026 | 3 |
Airframe · Bombardier BD-100-1A10
AD 2026-13-02NavigationAD 2026-02-06Flight controlsAD 2026-01-07Time Limits/Maintenance ChecksInformation bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Bombardier BD-100-1A10
SAIB AIR-22-02R1Pitot/Static Anti-Ice SystemSAIB NM-18-32R1Electrical Power - Direct Current Power CenterNTSB investigations
No NTSB investigations matched to N739QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bombardier BD-100-1A10 aircraft
FAA incident reports
No FAA accident or incident reports matched to N739QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Bombardier BD-100-1A10 aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026010206365Actuator · faultedUPON BRINGING THE GEAR UP ON TAKEOFF, WE GOT A GEAR DISAGREE AMBER CAS MESSAGE. LEFT MAIN GEAR STAYED DOWN. NOSE AND RIGHT MAIN GEAR WENT UP. ACCOMPLISHED THE GEAR DISAGREE QRH. R & R LT STAY ACTUATOR IAW AMM 32-32-07. R &R LT BRACE ATTACH PIN IAW AMM 32-32-0SDR DXTA2025121506096Apu · contaminatedDURING DESCENT THROUGH 9000 FEET, BOTH PILOTS NOTICED STRONG, EXHAUST SMELL IN THE COCKPIT. ENVIRONMENTAL WERE TRANSFERRED TO THE APU, WHICH MINIMIZED THE SMELL MOMENTARILY. THE SMELL WAS CLOSER TO EXHAUST, NOT DEICING FLUID, NOT ACRID, OR ELECTRICAL. CORRECTISDR DXTA2025102405390Pump · defectiveRIGHT HYD RESERVOIR DUMPED ALL FLUID TO 0% AT FL430. CYAN FLAPS RATE LOW AND R HYD ENG PUMP FAIL ILLUMINATED. AMBER R HYD LOW AND SPILER FAULT ILLUMINATED WHEN FLAPS EXTENDED VIA ALTN FLAPS. POST FLIGHT SHOWED HYD FLUID DRIPPING FROM BOTH R ENGINE LOWER WEEP HSDR 2025FA0000459Skin · corrodedCORROSION WAS FOUND ON THE LOWER FUSELAGE SKIN NEAR FS 779 NEAR STR 22L & 23L, NOMINAL THICKNESS 0.060 IN, MINIMUM 0.035 IN. MATERIAL TYPE 2024-T42 PER AMS-QQ-A-250''5.SDR DXTA2025013102175Door · obstructedMAIN DOOR: MAIN CABIN DOOR WILL NOT OPEN. DOOR HANDLE WILL COME OUT ABOUT HALF WAY BUT THE DOOR WILL NOT RELEASE. CORRECTIVE ACTION: MED CURTAIN MOVED OUT OF THE WAY. OPS CHECK GOOD. IAW CL350 AMM 52-11-00.SDR DXTA2024122401637Brake Assy · wornON LANDING, RIGHT BRAKE FELT SPONGEE. RIGHT OUTBOARD BRAKE SMOKING AFTER LANDING. APPEARS TO BE FLUID ON THE INBOARD SIDE OF RIGHT OUTBAORD TIRE. ##4 BRAKE WTL. INSTALLED OVERHAULED #4 RIGHT MAIN BRAKE ASSEMBLY. IAW MM 32-43-13-400-801. PERFORMED BRAKE BLEEDISDR DXTA2024091200480Engine · power lossAT ROTATION, RED CAS & MASTER WARNING. ENG ROLLED BACK, CAME BACK UP, 2ND IDENTICAL CAS FOLLOWED BY ROLL BACK AGAIN. ENG DID NOT HAVE POWER CONTROL FOR ROUGHLY 1 MIN. REMOVED ENG SN: PL36679 DUE TO ITI OVER TEMP OF L 197 DEGREES. INSTALLED REPAIRED ENG SN: PLSDR DXTA2024091200481Landing Gear · no discrepancyOVERWEIGHT LANDING: LANDED OVERWEIGHT DUE TO EMERGENCY AND ENGINE FAILURE. PLENTY OF RUNWAY AND GENTLE ON BRAKES. BASED ON THE AMM TASK 05-51-01-210-801 STEP 1.C(3)(A) AND THE INFORMATION PROVIDED FOR THE EVENT (AIRCRAFT LANDING WEIGHT AND RATE OF DESCENT) IT SDR DXTA2024081500197Bypass Valve · defectiveRIGHT HYDRAULIC TEMP HI YELLOW CAS CAME INTO VIEW WHILE IN DESCENT INTO KAUS. RIGHT HYDRAULIC TEMP READ 100 DEGREES CELSIUS PER HYDRAULIC SCHEMATIC DISPLAY. TEMP WENT DOWN TO 70 CELSIUS AFTE RH HYD SOV WAS CLOSED AS PER THE QRH. RAN BOTH ENGINES AND HYD PUMPS SDR DXTA2023070390020Unknown · unknownCOCKPIT ODOR: APPROX 15 MIN FROM DESTINATION BEGAN TO SMELL BURRING ODOR. NO VISIBLE SMOKE. APU WAS OFF ENGINE BLEEDS ON. ODOR REMAINED FOR DURATION OFF FLIGHT. WE LANDED WITH APU OFF, DURING TAXI IN STARTED APU AND TRANSFERRED BLEEDS. WE FELT THE AIR FROSDR DXTA2020121304462Warning Message · false activationCYAN FIRE SYSTEM FAULT MESSAGE DISPLAYED ON EICAS FOR MOST OF THE FLIGHT. RESEARCHED FIRE SYSTEM AND RESEARCHED LT ENGINE FIRE LOOP B B3-008146 ON SAMRTFIX. GAINED ACCESS TO FIREX BOX, DISCONNECTED A91P2, AND PERFORMED A CONTINUITY CHECK OF PINS 10 AND 11. SDR DXTA2019021802039Proximity Switch · defectiveAT FL320 AND CLIMBING THE AMBER EMERGENCY EXIT CAS LIGHT ILLUMINATED. AFTER DESCENDING BELOW FL280 THE LIGHT WENT OUT. REMOVED & REPLACED EMERGENCY EXIT DOOR PROX SWITCH IAW CL-350 M/M 52-71-21. OPS CHK GOOD.
Reports on N739QS not matched to an aircraft · 4
They name N739QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2013082605485Wheel · vibrationWHEN RETRACTING GEAR AFTER NORMAL TAKEOFF, NOSE WHEEL WOBBLES AND CAUSES A VIBRATION ON NOSE OF ACFT FOR 10-12 SECONDS.SDR DXTA2010060304109Brake · malfunctionedWHEN BRAKES ARE APPLIED DURING TAXI THERE IS A INTERMITTENT LOUD BANG IN THE NOSE OF THE ACFT WITH THE BRAKES GRABBING. BLED ALL 4 BRAKES AND TAXI CHECKED ACFT, NO DISCREPANCIES NOTED. SERVICED RT HYD RESERVOIR WITH FLUID AFTER BRAKE BLEED. ALL WORK DONE IAWSDR DXTA200811223367Controller · inoperativeIMMEDIATELY AFTER TAKEOFF, POWER SET, WE GOT THE RED DITCH LIGHT THE YELLOW AUTO PRESS FAULT LIGHT AND THE FOLLOWING EICAS MESSAGES CABIN ALT HIGH AUTO PRESS R FADEC MINOR PRESS MONITOR ADDITIONALLY THE CABIN OXYGEN MASK DEPLOYED. INTERAGATED MDC AND FOUND CPC
STCs that may be installed · 141
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 141 STCs